Aircraft Engineering and Aerospace Technology: Volume 17 Issue 10
Strapline:
An International JournalTable of contents
Our two‐hundredth number
HAD conditions in England returned to the pre‐war normal we should have signalized the appearance of this our two‐hundredth number by producing a “bumper” issue with something…
The Scientific Civil Service: Reorganization and Recruitment during the Reconstruction Period
The Government have decided that the Scientific Civil Service is to be reorganized. They are deeply conscious of the contribution made by science towards the winning of the war, a…
Standard Atmospheric Conditions
G.B. SaksenaALL aircraft and aero‐engine performance calculations are reduced to an agreed Standard Atmosphere defined by the International Commission on Air Navigation in order that direct…
High‐Lift Devices and Tailless Aeroplanes
A.R. WeylTHE present conception of the air flow over aeroplane wings assumes that, in general, the flow pattern conforms closely to that of potential flow (i.e. the inviscid…
Some Books Recently Received
The need of codifying a branch of law, of reducing it to the confines of one book, has always produced the author sufficiently experienced and courageous for the task.
Modern Aeroplane Types: Four‐engined Long‐range Transport Aeroplane with Pressure Cabin
THE Tudor, while still frankly a design that has had to be produced under the restrictions of war, is a far closer approach to the air liner of post‐war years than is anything…
Research Reports and Memoranda
The first solution of the problem of finding the wall‐interference of a wind tunnel of elliptic cross‐section was given by Sanuki and Tani. The method used in that investigation…
An Analysis of Wear of Aero Engine Parts
W.N. TwelvetreesALL machines, particularly modern machines, are constructed and operated with the general understanding that they will at some time wear out. Wear is combated in many ways but…
Testing Electrical Installations in Aircraft
Arthur ClarkMOST aircraft manufacturers would like to be able to check completely the functioning of all electrical installations while the aircraft is still in the rigging shop and without…
U.S. Patent Specifications
A temperature control for aircraft instruments comprising in combination an aircraft engine having a hot oil sump and a relatively cool oil sump, conduits from said sumps, a…
ISSN:
0002-2667Online date, start – end:
1929Copyright Holder:
Emerald Publishing LimitedOpen Access:
hybridEditor:
- Prof Phil Webb